|
US2015064026A1
|
|
Motor cooling system manifold
|
|
US2013174576A1
|
|
Turbomachine component alignment
|
|
US2013177389A1
|
|
Turbomachine component temperature control
|
|
US2013112277A1
|
|
Compact turbomachine system with improved slug flow handling
|
|
US2013098037A1
|
|
Advanced super-critical CO2 expander-generator
|
|
US2013078118A1
|
|
Sub-frame integration of motor-compressor systems
|
|
US2014109574A1
|
|
Combined heat exchanger expander mounting system
|
|
US2014190172A1
|
|
Parallel cascaded cycle gas expander
|
|
US2015184539A1
|
|
Compact compression system with integral heat exchangers
|
|
US2013160876A1
|
|
Flush-enabled controlled flow drain
|
|
US2011252779A1
|
|
Energy conversion system with duplex radial flow turbine
|
|
US2011084563A1
|
|
Auxiliary bearing system with plurality of inertia rings for magnetically supported rotor system
|
|
US2011061536A1
|
|
Density-based compact separator
|
|
US2010247299A1
|
|
High pressure casing access cover
|
|
US2010239437A1
|
|
Fluid channeling device for back-to-back compressors
|
|
US2010239419A1
|
|
Slidable cover for casing access port
|
|
US2010183438A1
|
|
Compact shaft support device for turbomachines
|
|
US2009321343A1
|
|
Dual body drum for rotary separators
|
|
US2009324391A1
|
|
Rotary separator and shaft coupler for compressors
|
|
US2009322033A1
|
|
Shaft isolation seal
|
